View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 58145U 26145.42865286 +.00000000 +00000-0 +17463-3 0 00009
2 58145 34.9892 150.6018 0007551 199.9980 160.0438 15.17526235 03
| Epoch (UTC): | 25 May 2026 10:17:15 |
| Eccentricity: | 0.0007551 |
| inclination: | 34.9892° |
| perigee height: | 508 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 150.6018° |
| argument of perigee: | 199.9980° |
| revolutions per day: | 15.17526235 |
| mean anomaly at epoch: | 160.0438° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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